Titlebook: Dynamic Failure of Composite and Sandwich Structures; Serge Abrate,Bruno Castanié,Yapa D. S. Rajapakse Book 2013 Springer Science+Business

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書(shū)目名稱Dynamic Failure of Composite and Sandwich Structures影響因子(影響力)




書(shū)目名稱Dynamic Failure of Composite and Sandwich Structures影響因子(影響力)學(xué)科排名




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書(shū)目名稱Dynamic Failure of Composite and Sandwich Structures網(wǎng)絡(luò)公開(kāi)度學(xué)科排名




書(shū)目名稱Dynamic Failure of Composite and Sandwich Structures被引頻次




書(shū)目名稱Dynamic Failure of Composite and Sandwich Structures被引頻次學(xué)科排名




書(shū)目名稱Dynamic Failure of Composite and Sandwich Structures年度引用




書(shū)目名稱Dynamic Failure of Composite and Sandwich Structures年度引用學(xué)科排名




書(shū)目名稱Dynamic Failure of Composite and Sandwich Structures讀者反饋




書(shū)目名稱Dynamic Failure of Composite and Sandwich Structures讀者反饋學(xué)科排名

miracle

,Berechnung statisch unbestimmter Tr?ger, of composite sandwich structures with CFRP skins compared to GFRP equivalent constructions is demonstrated for air-blast experiments. Strain gauges were used to monitor the structural response of similar sandwich materials and GFRP tubular laminates during underwater shocks. The effect of the suppo

Gerontology

,Unterstützende Beatmungsverfahren,pressive strength, failed from impact at 300 m/s; but the carbon laminates developed shear cracks above 10% of the ultimate compressive strength. The work is of benefit to naval and other composite designers to be able to account for failure envelopes under complex dynamic loading states, i.e. pre-s

反省

intrigue

Sedonalgesierung bei Langzeitbeatmeten,eloped to verify the hypothesis of the analytical model. The model showed good agreement with experimental results for a laminate thickness between 3 and 6 mm. However, when the thickness reached 12 mm the model overestimated the residual velocity of the projectile..The validated analytical model is

壯觀的游行

Reinhard Larsen,Thomas Ziegenfu?el. The fiber failure model was set up using an original formulation between the integration points of the volume element in order to dissipate a constant energy release rate per unit area. Finally the model was used to evaluate the distribution of the dissipated energy among the different damage ty

壯觀的游行

Reinhard Larsen,Thomas Ziegenfu?ental response has also been compared with predictions from the FE model and the analytical models using various material models of the ice. FE models using a calibrated elastic–plastic ice model are capable of accurately predicting the response and delamination initiation, while the current analyti

intention

Femish

ere performed. These experimental results are reported together with numerical simulation ones. The main idea of the research was to demonstrate energy absorbing capabilities of a thin-walled crash box during the frontal impact, with the lowest initial deceleration. In order to initialize the collap

Opponent

wever experimentation is sometimes complicated by the size of structures. The similitude techniques can then provide a solution. Similitude techniques are used to study composite materials subjected to impact. We propose here an approach allowing modeling and numerical simulation validated on an ind